[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 19th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2011/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -409040
78 A = 6730021
64 meter
Y = -6136276
21 meter E =
0016016
Z = 2715091
39 I = 51
97774
XDOT = 5022
558487 Wp = 102
84030
YDOT = -2648
664016 meter/sec RA = 106
38051 deg
ZDOT = -5207
404848 TA = 46
31699
MA = 46
18438
Ha = 191
523 n
mi
Hp = 183
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1341997
32 X = -353583
00
Y = -20132139
81 feet Y = -6140540
17 meter
Z = 8907780
14 Z = 2713239
18
XDOT = 16478
210260 XDOT = 5077
100090
YDOT = -8689
842571 feet/sec YDOT = -2592
193959 meter/sec
ZDOT = -17084
661575 ZDOT = -5182
872295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9917307
42 X = -3022795
30
Y = -17575037
35 feet Y = -5356871
39 meter
Z = 8900428
80 Z = 2712850
70
XDOT = 9949
745902 XDOT = 3032
682551
YDOT = -14252
976994 feet/sec YDOT = -4344
307388 meter/sec
ZDOT = -16985
351503 ZDOT = -5177
135138
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11108
53726012
00016717 00000-0 10270-3 0 9004
2 25544 51
6398 107
0756 0002417 111
7645 248
3776 15
73633813 31516
Satellite: ISS
Catalog Number: 25544
Epoch time: 11108
53726012 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 107
0756 deg
Eccentricity:
0002417
Arg of perigee: 111
7645 deg
Mean anomaly: 248
3776 deg
Mean motion: 15
73633813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 294
Coasting Arc #2 (Orbit 3166)
---------------------------------------
Vector Time (GMT): 2011/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4138816
53 A = 6724482
88 meter
Y = 2820335
25 meter E =
0011399
Z = 4480637
53 I = 51
96657
XDOT = -1193
658220 Wp = 113
32536
YDOT = -6893
648374 meter/sec RA = 101
31730 deg
ZDOT = 3225
761058 TA = 304
50783
MA = 304
61542
Ha = 191
511 n
mi
Hp = 183
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13578794
37 X = -4191812
90
Y = 9253068
41 feet Y = 2773756
21 meter
Z = 14700254
37 Z = 4460402
11
XDOT = -3916
201510 XDOT = -1132
153811
YDOT = -22616
956608 feet/sec YDOT = -6906
652671 meter/sec
ZDOT = 10583
205572 ZDOT = 3220
111627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8112679
57 X = -2472744
73
Y = 14373230
96 feet Y = 4380960
80 meter
Z = 14618312
90 Z = 4455661
77
XDOT = -12590
590067 XDOT = -3837
611852
YDOT = -17883
496904 feet/sec YDOT = -5450
889856 meter/sec
ZDOT = 10560
525819 ZDOT = 3218
848270
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11109
55332643
00016717 00000-0 10270-3 0 9011
2 25544 51
6394 101
8604 0002355 118
1594 241
9807 15
73666871 31672
Satellite: ISS
Catalog Number: 25544
Epoch time: 11109
55332643 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 101
8604 deg
Eccentricity:
0002355
Arg of perigee: 118
1594 deg
Mean anomaly: 241
9807 deg
Mean motion: 15
73666871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3167
Checksum: 307
Coasting Arc #3 (Orbit 3181)
---------------------------------------
Vector Time (GMT): 2011/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1644930
24 A = 6729394
15 meter
Y = 5849737
39 meter E =
0006350
Z = -2895668
71 I = 51
98874
XDOT = -4398
607583 Wp = 83
11807
YDOT = 3746
808243 meter/sec RA = 96
16123 deg
ZDOT = 5080
676198 TA = 243
78949
MA = 243
85478
Ha = 191
380 n
mi
Hp = 183
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5396752
76 X = 1593461
91
Y = 19192051
81 feet Y = 5867844
28 meter
Z = -9500225
41 Z = -2887802
45
XDOT = -14431
127240 XDOT = -4464
859489
YDOT = 12292
677963 feet/sec YDOT = 3697
249820 meter/sec
ZDOT = 16668
885163 ZDOT = 5059
146649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13684324
94 X = 4170982
24
Y = 14518941
61 feet Y = 4425373
40 meter
Z = -9468561
75 Z = -2886017
62
XDOT = -6171
542897 XDOT = -1881
086275
YDOT = 16608
667454 feet/sec YDOT = 5062
321840 meter/sec
ZDOT = 16581
668745 ZDOT = 5054
092633
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11110
50585581
00016717 00000-0 10270-3 0 9020
2 25544 51
6397 96
9712 0002461 119
3483 240
7926 15
73704503 31828
Satellite: ISS
Catalog Number: 25544
Epoch time: 11110
50585581 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 96
9712 deg
Eccentricity:
0002461
Arg of perigee: 119
3483 deg
Mean anomaly: 240
7926 deg
Mean motion: 15
73704503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3182
Checksum: 302
Coasting Arc #4 (Orbit 3197)
---------------------------------------
Vector Time (GMT): 2011/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3521837
81 A = 6724483
86 meter
Y = -3664683
26 meter E =
0010798
Z = -4413047
76 I = 51
97513
XDOT = 2505
117191 Wp = 79
87467
YDOT = 6448
767838 meter/sec RA = 91
09845 deg
ZDOT = -3361
039056 TA = 156
45817
MA = 156
40871
Ha = 191
260 n
mi
Hp = 183
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11554585
99 X = 3583993
19
Y = -12023239
04 feet Y = -3624952
26 meter
Z = -14478503
14 Z = -4395787
69
XDOT = 8218
888422 XDOT = 2449
147088
YDOT = 21157
374797 feet/sec YDOT = 6476
468741 meter/sec
ZDOT = -11027
031022 ZDOT = -3349
004851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4513491
28 X = 1375712
14
Y = -16115701
85 feet Y = -4912065
92 meter
Z = -14408550
87 Z = -4391726
30
XDOT = 16182
263582 XDOT = 4932
353940
YDOT = 14332
768674 feet/sec YDOT = 4368
627892 meter/sec
ZDOT = -10978
529629 ZDOT = -3346
255831
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11111
52185220
00016717 00000-0 10270-3 0 9030
2 25544 51
6400 91
7547 0002419 124
4966 235
6426 15
73761681 31983
Satellite: ISS
Catalog Number: 25544
Epoch time: 11111
52185220 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 91
7547 deg
Eccentricity:
0002419
Arg of perigee: 124
4966 deg
Mean anomaly: 235
6426 deg
Mean motion: 15
73761681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3198
Checksum: 297
Coasting Arc #5 (Orbit 3213)
---------------------------------------
Vector Time (GMT): 2011/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2712194
38 A = 6728834
24 meter
Y = -5383072
19 meter E =
0015281
Z = 2974007
46 I = 51
99008
XDOT = 3606
512058 Wp = 101
50203
YDOT = -4600
521858 meter/sec RA = 85
94122 deg
ZDOT = -5019
535521 TA = 44
33349
MA = 44
21122
Ha = 191
097 n
mi
Hp = 183
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8898275
54 X = -2666245
49
Y = -17660997
99 feet Y = -5413144
78 meter
Z = 9757242
32 Z = 2960943
01
XDOT = 11832
388641 XDOT = 3682
071987
YDOT = -15093
575651 feet/sec YDOT = -4559
769000 meter/sec
ZDOT = -16468
292393 ZDOT = -5001
831664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16475208
91 X = -5021643
67
Y = -10985591
93 feet Y = -3348408
42 meter
Z = 9704545
16 Z = 2957945
36
XDOT = 2179
011914 XDOT = 664
162831
YDOT = -17806
497489 feet/sec YDOT = -5427
420435 meter/sec
ZDOT = -16396
502946 ZDOT = -4997
654098
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11112
53781099
00016717 00000-0 10270-3 0 9049
2 25544 51
6401 86
5392 0002239 128
2086 231
9279 15
73837750 32144
Satellite: ISS
Catalog Number: 25544
Epoch time: 11112
53781099 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 86
5392 deg
Eccentricity:
0002239
Arg of perigee: 128
2086 deg
Mean anomaly: 231
9279 deg
Mean motion: 15
73837750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3214
Checksum: 307
Coasting Arc #6 (Orbit 3229)
---------------------------------------
Vector Time (GMT): 2011/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2755142
26 A = 6724218
81 meter
Y = 4315241
32 meter E =
0011631
Z = 4353025
61 I = 51
97269
XDOT = -3667
375710 Wp = 114
36471
YDOT = -5831
809887 meter/sec RA = 80
87988 deg
ZDOT = 3448
157172 TA = 300
95271
MA = 301
06696
Ha = 190
928 n
mi
Hp = 183
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9039180
64 X = -2824337
53
Y = 14157615
88 feet Y = 4284044
64 meter
Z = 14281580
07 Z = 4339473
18
XDOT = -12032
072541 XDOT = -3618
641235
YDOT = -19133
234538 feet/sec YDOT = -5872
548311 meter/sec
ZDOT = 11312
851613 ZDOT = 3430
459297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -705889
12 X = -215155
00
Y = 16828970
61 feet Y = 5129470
24 meter
Z = 14226590
32 Z = 4336264
73
XDOT = -18890
457441 XDOT = -5757
811428
YDOT = -10328
450023 feet/sec YDOT = -3148
111567 meter/sec
ZDOT = 11241
421735 ZDOT = 3426
385345
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11113
55373201
00016717 00000-0 10270-3 0 9055
2 25544 51
6408 81
3239 0002250 137
2813 222
8525 15
73920190 32307
Satellite: ISS
Catalog Number: 25544
Epoch time: 11113
55373201 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 81
3239 deg
Eccentricity:
0002250
Arg of perigee: 137
2813 deg
Mean anomaly: 222
8525 deg
Mean motion: 15
73920190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3230
Checksum: 266
Coasting Arc #7 (Orbit 3244)
---------------------------------------
Vector Time (GMT): 2011/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3655277
37 A = 6728459
25 meter
Y = 4774269
35 meter E =
0005834
Z = -3024624
96 I = 51
98091
XDOT = -2691
605503 Wp = 91
03259
YDOT = 5210
779996 meter/sec RA = 75
72008 deg
ZDOT = 4980
323811 TA = 234
18844
MA = 234
24267
Ha = 190
866 n
mi
Hp = 183
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11992379
83 X = 3616311
94
Y = 15663613
37 feet Y = 4814927
05 meter
Z = -9923310
25 Z = -3006962
28
XDOT = -8830
726717 XDOT = -2773
866827
YDOT = 17095
734896 feet/sec YDOT = 5180
220823 meter/sec
ZDOT = 16339
645048 ZDOT = 4967
048285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18445370
09 X = 5622148
80
Y = 7095397
46 feet Y = 2162677
15 meter
Z = -9851989
72 Z = -3002886
47
XDOT = 1798
673744 XDOT = 548
235757
YDOT = 17899
759171 feet/sec YDOT = 5455
846595 meter/sec
ZDOT = 16285
737993 ZDOT = 4963
892940
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11114
50612580
00016717 00000-0 10270-3 0 9068
2 25544 51
6407 76
4334 0002257 136
1146 224
0197 15
73927841 32456
Satellite: ISS
Catalog Number: 25544
Epoch time: 11114
50612580 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 76
4334 deg
Eccentricity:
0002257
Arg of perigee: 136
1146 deg
Mean anomaly: 224
0197 deg
Mean motion: 15
73927841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3245
Checksum: 288
Coasting Arc #8 (Orbit 3260)
---------------------------------------
Vector Time (GMT): 2011/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1959495
09 A = 6723922
32 meter
Y = -4731787
54 meter E =
0009928
Z = -4366052
00 I = 51
95853
XDOT = 4635
824341 Wp = 81
45027
YDOT = 5086
371057 meter/sec RA = 70
65605 deg
ZDOT = -3437
039838 TA = 154
01113
MA = 153
96125
Ha = 190
692 n
mi
Hp = 183
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6428789
67 X = 2033470
62
Y = -15524237
34 feet Y = -4709461
68 meter
Z = -14324317
59 Z = -4356353
10
XDOT = 15209
397444 XDOT = 4595
299476
YDOT = 16687
569085 feet/sec YDOT = 5137
985051 meter/sec
ZDOT = -11276
377420 ZDOT = -3414
617553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2809568
89 X = -856356
60
Y = -16600162
80 feet Y = -5059729
62 meter
Z = -14284896
70 Z = -4354036
51
XDOT = 20626
287093 XDOT = 6286
892306
YDOT = 6120
089369 feet/sec YDOT = 1865
403240 meter/sec
ZDOT = -11185
807167 ZDOT = -3409
434024
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11115
52197428
00016717 00000-0 10270-3 0 9071
2 25544 51
6414 71
2165 0002225 141
5569 218
5753 15
74007689 32617
Satellite: ISS
Catalog Number: 25544
Epoch time: 11115
52197428 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 71
2165 deg
Eccentricity:
0002225
Arg of perigee: 141
5569 deg
Mean anomaly: 218
5753 deg
Mean motion: 15
74007689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3261
Checksum: 302
Coasting Arc #9 (Orbit 3276)
---------------------------------------
Vector Time (GMT): 2011/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4423882
52 A = 6728202
23 meter
Y = -4091630
88 meter E =
0014844
Z = 2976080
61 I = 51
96239
XDOT = 1770
829248 Wp = 103
51019
YDOT = -5575
252491 meter/sec RA = 65
49512 deg
ZDOT = -5015
413772 TA = 42
27965
MA = 42
16531
Ha = 190
607 n
mi
Hp = 183
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14514050
27 X = -4392257
56
Y = -13423985
84 feet Y = -4140924
53 meter
Z = 9764043
99 Z = 2954666
35
XDOT = 5809
807243 XDOT = 1857
405089
YDOT = -18291
510796 feet/sec YDOT = -5554
966041 meter/sec
ZDOT = -16454
769593 ZDOT = -5006
600691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19552562
26 X = -5959620
98
Y = -3200075
79 feet Y = -975383
10 meter
Z = 9677521
89 Z = 2949708
67
XDOT = -5355
989206 XDOT = -1632
505510
YDOT = -17101
779765 feet/sec YDOT = -5212
622472 meter/sec
ZDOT = -16418
898575 ZDOT = -5004
480286
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11116
53778443
00016717 00000-0 10270-3 0 9086
2 25544 51
6417 65
9999 0002171 146
4925 213
6376 15
74066790 32777
Satellite: ISS
Catalog Number: 25544
Epoch time: 11116
53778443 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 65
9999 deg
Eccentricity:
0002171
Arg of perigee: 146
4925 deg
Mean anomaly: 213
6376 deg
Mean motion: 15
74066790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3277
Checksum: 337
Coasting Arc #10 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2011/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1143630
39 A = 6723373
87 meter
Y = 4955212
07 meter E =
0011087
Z = 4392623
53 I = 51
93384
XDOT = -5457
771844 Wp = 118
47279
YDOT = -4262
129184 meter/sec RA = 60
42905 deg
ZDOT = 3375
492346 TA = 297
65398
MA = 297
76648
Ha = 190
370 n
mi
Hp = 183
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3752068
22 X = -1220294
11
Y = 16257257
43 feet Y = 4941994
79 meter
Z = 14411494
53 Z = 4386881
40
XDOT = -17906
075604 XDOT = -5426
103803
YDOT = -13983
363466 feet/sec YDOT = -4322
984127 meter/sec
ZDOT = 11074
449955 ZDOT = 3349
055543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6002101
56 X = 1829440
56
Y = 15589285
47 feet Y = 4751614
21 meter
Z = 14388070
24 Z = 4385483
81
XDOT = -21590
655330 XDOT = -6580
831745
YDOT = -1844
883178 feet/sec YDOT = -562
320393 meter/sec
ZDOT = 10967
611823 ZDOT = 3342
928084
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11117
55355455
00016717 00000-0 10270-3 0 9094
2 25544 51
6423 60
7833 0002258 155
7394 204
3876 15
74150921 32933
Satellite: ISS
Catalog Number: 25544
Epoch time: 11117
55355455 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 60
7833 deg
Eccentricity:
0002258
Arg of perigee: 155
7394 deg
Mean anomaly: 204
3876 deg
Mean motion: 15
74150921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 311
Coasting Arc #11 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2011/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5074686
76 A = 6728131
20 meter
Y = 3340663
53 meter E =
0004932
Z = -2894619
11 I = 51
93356
XDOT = -872
896246 Wp = 88
73092
YDOT = 5717
431057 meter/sec RA = 55
26526 deg
ZDOT = 5075
639177 TA = 238
15428
MA = 238
20230
Ha = 190
264 n
mi
Hp = 183
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16649234
78 X = 5051015
25
Y = 10960182
18 feet Y = 3397279
30 meter
Z = -9496781
87 Z = -2870023
80
XDOT = -2863
832829 XDOT = -961
421419
YDOT = 18757
975909 feet/sec YDOT = 5707
175013 meter/sec
ZDOT = 16652
359503 ZDOT = 5071
183395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19967100
82 X = 6085972
33
Y = -718206
29 feet Y = -218909
28 meter
Z = -9397368
93 Z = -2864318
05
XDOT = 8376
784091 XDOT = 2553
243791
YDOT = 15562
204230 feet/sec YDOT = 4743
359849 meter/sec
ZDOT = 16634
106664 ZDOT = 5070
075711
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11118
50580603
00016717 00000-0 10270-3 0 9107
2 25544 51
6421 55
8918 0002120 158
1397 201
9857 15
74166713 33083
Satellite: ISS
Catalog Number: 25544
Epoch time: 11118
50580603 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 55
8918 deg
Eccentricity:
0002120
Arg of perigee: 158
1397 deg
Mean anomaly: 201
9857 deg
Mean motion: 15
74166713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 294
Coasting Arc #12 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2011/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 419618
06 A = 6722715
55 meter
Y = -4994933
89 meter E =
0009975
Z = -4489101
71 I = 51
89889
XDOT = 6109
554641 Wp = 81
68428
YDOT = 3396
410088 meter/sec RA = 50
19430 deg
ZDOT = -3212
658004 TA = 156
28735
MA = 156
24136
Ha = 190
101 n
mi
Hp = 183
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1376699
67 X = 497248
60
Y = -16387578
37 feet Y = -4989807
55 meter
Z = -14728023
98 Z = -4486874
46
XDOT = 20044
470606 XDOT = 6086
727894
YDOT = 11143
077717 feet/sec YDOT = 3464
603101 meter/sec
ZDOT = -10540
216548 ZDOT = -3183
033104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8524477
54 X = -2598260
75
Y = -14073115
61 feet Y = -4289485
64 meter
Z = -14718811
67 Z = -4486293
80
XDOT = 21774
717065 XDOT = 6636
933761
YDOT = -2306
883322 feet/sec YDOT = -703
138036 meter/sec
ZDOT = -10420
458747 ZDOT = -3176
155826
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11119
52150207
00016717 00000-0 10270-3 0 9114
2 25544 51
6432 50
6740 0002160 161
2880 198
8363 15
74252467 33243
Satellite: ISS
Catalog Number: 25544
Epoch time: 11119
52150207 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 50
6740 deg
Eccentricity:
0002160
Arg of perigee: 161
2880 deg
Mean anomaly: 198
8363 deg
Mean motion: 15
74252467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 281
Coasting Arc #13 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2011/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5582206
60 A = 6728205
62 meter
Y = -2579989
67 meter E =
0014710
Z = 2710968
69 I = 51
89748
XDOT = 90
672025 Wp = 109
14817
YDOT = -5682
717974 meter/sec RA = 45
02954 deg
ZDOT = -5203
409354 TA = 40
01366
MA = 39
90537
Ha = 190
037 n
mi
Hp = 183
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18314326
13 X = -5566111
33
Y = -8464533
03 feet Y = -2642323
23 meter
Z = 8894254
22 Z = 2683889
16
XDOT = 297
480396 XDOT = 179
488052
YDOT = -18644
087840 feet/sec YDOT = -5681
207547 meter/sec
ZDOT = -17071
552999 ZDOT = -5202
752996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19740009
94 X = -6016755
03
Y = 4396633
62 feet Y = 1340093
93 meter
Z = 8784773
17 Z = 2677598
86
XDOT = -10659
434584 XDOT = -3248
995661
YDOT = -13634
615438 feet/sec YDOT = -4155
830785 meter/sec
ZDOT = -17068
662019 ZDOT = -5202
528184
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11120
53715930
00016717 00000-0 10270-3 0 9128
2 25544 51
6436 45
4567 0002184 167
5462 192
5755 15
74299816 33400
Satellite: ISS
Catalog Number: 25544
Epoch time: 11120
53715930 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 45
4567 deg
Eccentricity:
0002184
Arg of perigee: 167
5462 deg
Mean anomaly: 192
5755 deg
Mean motion: 15
74299816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3340
Checksum: 312
Coasting Arc #14 (Orbit 3355)
---------------------------------------
Vector Time (GMT): 2011/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 229309
10 A = 6721931
73 meter
Y = 4898408
31 meter E =
0009742
Z = 4593625
78 I = 51
85493
XDOT = -6644
038785 Wp = 126
29671
YDOT = -2502
396011 meter/sec RA = 39
95345 deg
ZDOT = 2990
073223 TA = 294
07930
MA = 294
18119
Ha = 189
793 n
mi
Hp = 183
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 752326
44 X = 152201
77
Y = 16070893
40 feet Y = 4900541
49 meter
Z = 15070950
72 Z = 4594552
44
XDOT = -21798
027511 XDOT = -6630
088164
YDOT = -8209
960667 feet/sec YDOT = -2576
615657 meter/sec
ZDOT = 9809
951519 ZDOT = 2957
829905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10476867
73 X = 3193349
28
Y = 12205251
16 feet Y = 3720160
55 meter
Z = 15074490
11 Z = 4594704
59
XDOT = -21352
496190 XDOT = -6508
240839
YDOT = 6333
112293 feet/sec YDOT = 1930
332627 meter/sec
ZDOT = 9679
578666 ZDOT = 2950
335577
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11121
55277695
00016717 00000-0 10270-3 0 9133
2 25544 51
6438 40
2389 0002248 173
4942 186
6250 15
74369160 33568
Satellite: ISS
Catalog Number: 25544
Epoch time: 11121
55277695 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 40
2389 deg
Eccentricity:
0002248
Arg of perigee: 173
4942 deg
Mean anomaly: 186
6250 deg
Mean motion: 15
74369160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3356
Checksum: 315
Coasting Arc #15 (Orbit 3370)
---------------------------------------
Vector Time (GMT): 2011/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5992511
12 A = 6728355
75 meter
Y = 1786346
12 meter E =
0004337
Z = -2485000
99 I = 51
85319
XDOT = 570
822069 Wp = 70
33479
YDOT = 5508
141891 meter/sec RA = 34
78668 deg
ZDOT = 5344
998686 TA = 261
65675
MA = 261
70592
Ha = 189
649 n
mi
Hp = 183
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19660469
55 X = 5984162
37
Y = 5860715
63 feet Y = 1853311
36 meter
Z = -8152890
37 Z = -2455909
13
XDOT = 1872
775816 XDOT = 483
221066
YDOT = 18071
331662 feet/sec YDOT = 5514
035317 meter/sec
ZDOT = 17536
084929 ZDOT = 5347
559051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18967692
66 X = 5781352
72
Y = -7938080
55 feet Y = -2419526
95 meter
Z = -8035246
39 Z = -2449143
10
XDOT = 12228
670155 XDOT = 3727
298663
YDOT = 11489
025944 feet/sec YDOT = 3501
855108 meter/sec
ZDOT = 17546
199228 ZDOT = 5348
081525
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11122
50488391
00016717 00000-0 10270-3 0 9147
2 25544 51
6444 35
3469 0002204 178
5277 181
5893 15
74424081 33716
Satellite: ISS
Catalog Number: 25544
Epoch time: 11122
50488391 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 35
3469 deg
Eccentricity:
0002204
Arg of perigee: 178
5277 deg
Mean anomaly: 181
5893 deg
Mean motion: 15
74424081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3371
Checksum: 307
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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